Method for depositing zirconium oxide on a substrate

- General Electric

An improved method for depositing zirconium oxide from a zirconium oxide source onto a substrate by means of physical vapor deposition is described. The method includes the step of adding zirconium metal to the zirconium oxide source, which is usually in the form of a cylindrical ingot. The zirconium metal is present in an amount sufficient to chemically bond with a substantial portion of oxygen which would otherwise be freed from the oxide source, as both the zirconium metal and the zirconium oxide source are evaporated during physical vapor deposition. The invention is especially suited for EB-PVD techniques, in which an electron beam is used to evaporate the zirconium metal and the zirconium oxide source during physical vapor deposition. In one embodiment, the zirconium metal comprises a tube which surrounds and contacts at least a portion of the outer surface of the ingot. In another embodiment, the zirconium metal is in the form of a rod inserted in a cavity within the ingot.

Skip to:  ·  Claims  ·  References Cited  · Patent History  ·  Patent History

Claims

1. An improved method for depositing zirconium oxide from a zirconium oxide source onto a substrate by means of physical vapor deposition, comprising the step of adding zirconium metal to the zirconium oxide source by further using the zirconium metal as an evaporation source adjacent to the zirconium oxide source.

2. The method of claim 1, wherein the zirconium oxide source is in the form of an ingot, and the zirconium metal comprises a tube which surrounds and contacts at least a portion of the outer surface of the ingot.

3. The method of claim 1, wherein the zirconium metal is present in an amount sufficient to chemically bond with a substantial portion of oxygen which would otherwise be freed from the oxide source, as both the zirconium metal and the zirconium oxide source are evaporated during physical vapor deposition.

4. The method of claim 1, wherein an electron beam is used to evaporate the zirconium metal and the zirconium oxide source during physical vapor deposition.

5. The method of claim 1, wherein the zirconium oxide source is in the form of an ingot, and the zirconium metal comprises a rod inserted in a cavity within the ingot.

6. The method of claim 1, wherein the zirconium oxide source is in a form selected from the group consisting of beads, powder, grains, and flakes.

7. The method of claim 6, wherein the zirconium metal is in the form of grains or beads.

8. The method of claim 1, wherein the physical vapor deposition is carried out in a vacuum chamber operating at a vacuum of about 0.005 millibar, and oxygen is added to the chamber during deposition to substantially maintain the pressure value.

9. The method of claim 1, wherein the substrate is made of a material comprising a superalloy.

10. The method of claim 9, wherein the superalloy is nickel-based.

11. The method of claim 1, wherein the substrate is a component of a turbine engine.

12. The method of claim 1 where the substrate has a bond coat layer first applied to the substrate to improve adhesion of subsequently applied zirconium oxide on the substrate.

13. The method of claim 12 where the bond coat is an aluminide or a nickel-base alloy different from the substrate or a MCrAlY coating, where M is selected from the group consisting of Fe, Ni, Co, and mixtures thereof.

14. The method of claim 1 where the zirconium oxide source is chemically stabilized by a material selected from the group consisting of yttrium oxide, calcium oxide, magnesium oxide, scandium oxide, and mixtures thereof.

15. A method for depositing evaporated zirconium oxide coatings onto a substrate, using a physical vapor deposition apparatus, comprising the steps of:

(a.) adding zirconium metal to an ingot of a zirconium oxide source material by using the zirconium metal as an evaporation source adjacent to the zirconium oxide source so that proportionate amounts of the metal and the oxide is exposed to an intense heat source which constitutes part of the apparatus;
(b.) evaporating a portion of the zirconium oxide source and zirconium metal by melting the surface of the ingot with the heat source, thereby forming a molten pool surrounding the ingot; and
(c.) depositing the evaporated material onto the substrate as a coating, wherein the ratio of zirconium metal to zirconium oxide source material is substantially maintained in a pre-selected proportion sufficient to substantially reduce or prevent the formation of gas bubbles in the molten pool.

16. The method of claim 15, wherein the intense heat source is an electron beam.

17. The method of claim 15, wherein the physical vapor deposition is carried out in a vacuum chamber operating at a vacuum of about 0.005 millibar, and oxygen is added to the chamber during deposition to substantially maintain the pressure value.

18. The method of claim 15, wherein the zirconium oxide source is in the form of a substantially cylindrical ingot, and the zirconium metal comprises a tube which surrounds and contacts at least a portion of the outer surface of the ingot.

19. The method of claim 15, wherein the zirconium oxide source is in the form of a substantially cylindrical ingot, and the zirconium metal comprises a rod inserted in a cavity within the ingot.

20. The method of claim 15, wherein the substrate is made of a material comprising a superalloy.

Referenced Cited
U.S. Patent Documents
5087477 February 11, 1992 Giggins, Jr.
5262245 November 16, 1993 Ulion et al.
5418003 May 23, 1995 Bruce et al.
5419971 May 30, 1995 Skelly et al.
5474809 December 12, 1995 Skelly et al.
5514482 May 7, 1996 Strangman
Other references
  • "Thermal Barrier Coatings-their Functional Benefits, Problems and Improvements in Mfg. and Quality" by P. Adam, T. Cosack, Proceedings of the Conf., London, UK, Jun. 16-18, 1993, p. 13.1-13.8. "Study of the Structure and Properities of Thick Vacuum Condensates of Nickel, Titanium, Tungsten, Aluminum Oxide and Zirconium Dioxide" by B.A. Movchan and A.V. Demchishin, Fiz. Metal. Metalloved., 28, No. 4, pp. 83-90, 1969. "Microstructural Development in Physical Vapour-deposited Partially Stabilized Zirconia Thermal Barrier Coatings" by Y.H. Sohn, R.R. Biederman and R.D. Sisson, Jr., Thin Solid Films, 250 (1994, pp. 1-7. "Microstructures of Y2O3-Stabilized ZrO2 Electron Beam-Physical Vapor Deposition Coatings on Ni-Base Superalloys", O. Unal, T.E. Mitchell and A.H. Heuer, J. Am. Ceramic Soc, 77 (4) (1994), pp. 984-992. "Mass Spectrometric Study of the Incongruent Step in the Evaporation of Lu2O3 and of ZrO2-Y2O3 and ZrO2-Lu2O3 Solid Solutions" by A.N. Belov, S.I. Loptain and G.A. Semenov, Russian Journal of Physical Chemistry 55 (4) 1981, pp. 524-528. "PVD Thermal Barrier Coating Applications and Process Development for Aircraft Engines" by D.V. Rigney, R. Viguie, D.J. Wortman and D.W. Skelly, pp. 135-149 NASA Workshop, Mar. 1995.
Patent History
Patent number: 5773078
Type: Grant
Filed: Jun 24, 1996
Date of Patent: Jun 30, 1998
Assignee: General Electric Company (Schenectady, NY)
Inventor: David William Skelly (Burnt Hills, NY)
Primary Examiner: Roy V. King
Attorneys: Noreen C. Johnson, Douglas E. Stoner
Application Number: 8/669,207
Classifications
Current U.S. Class: 427/1263; Electron Irradiation (e.g., E-beam Evaporation, Etc.) (427/566); 427/1262; Metal Base (427/405); 427/4192
International Classification: C23C 1424; B05D 306;